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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/75810


    Title: Missile Guidance Using Dual-Mode Seeker
    Authors: Ma, Der-Ming;Shiau, Jaw-Kuen;Ho, Ian
    Contributors: 淡江大學航空太空工程學系
    Keywords: Dual-mode seeker guidance;IR seeker;Kalman filter;Proportional navigation;RF seeker
    Date: 2011-08
    Issue Date: 2013-03-20 16:36:41 (UTC+8)
    Publisher: Manchester: Scholarlink Resource Centre Ltd.
    Abstract: This study developed an analytical method to quantitatively analyze the dual-mode seeker guidance performance. The method derives the seekers' measurement models and implements the Kalman filter. The study takes the RF/IR dual-mode seeker, which is proposed for advanced long/medium range air-to-air missiles, as the example. The two-dimensional guidance loop is used to illustrate the methodology and dimensionless equations are derived for generality. After discussing several missile-target scenarios, the results show that the developed scheme provides sufficiently accurate target information for missile guidance, not only for dual-mode seekers, but also when one of the seekers is jammed. The methodology developed in the study can also be applied to increase the accuracy of target tracking.
    Relation: Journal of Emerging Trends in Engineering and Applied Sciences 2(4), pp.636-642
    Appears in Collections:[航空太空工程學系暨研究所] 期刊論文

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